Sentence examples for leading edge flow from inspiring English sources

All of them improve the leading edge flow patterns and significantly affect the size of the predicted laminar separation bubble.

Many solutions have been proposed to solve this problem including, for example, leading edge spoilers, trailing edge deflectors, and leading edge flow diffusers.

Computed results at incidences of −10°,   −5°,   +5°,   +10° are used to illustrate the complete removal of leading edge flow-disturbance regions, thus minimizing the possibility of leading-edge separation bubbles, while concurrently minimizing the stagnation pressure drop from inlet to outlet.

Some physical and geometrical effects (surface catalysis of PM1000 and C SiC, wall temperature of the model leading edge, base flow) have been studied qualitatively through a series of simpler two-dimensional simulations.

At the leading edge, the flow experiences laminar separation-laminar reattachment state (1.5e3 < Re < 6e3), laminar separation-turbulence reattachment state (6e3 ≤ Re ≤ 8e4), and turbulence separation-turbulence reattachment flow state (Re > 8e4).

Aerodynamic studies in the 1960s demonstrated that the "vortex lift" phenomenon could be harnessed by highly swept wing configurations to reach higher angles of attack, using leading edge vortex flow off a slender lifting surface.

The increased flow at the leading edge leads to a severe adverse pressure gradient, resulting in immediate leading-edge flow separation.

The perturbation at leading edge and the flow separation at strut back lead to vorticity augmentation and velocity decrease at the vicinity of strut bound.

When we treated these cells with a 100 nM Cytochalasin D, we observed a large fraction of leading edge-localized GFP-Lpd850−1250aa immediately dissociate from the leading edge membrane and flow back with the actin cytoskeleton.

A common feature of the BBFs observed in the near-Earth plasma sheet at x∼−10R E is the occurrence of transient dipolarizations at the leading edge of the flows (Ohtani et al. 2004).

The numerical and experimental results show that the starting point of the TLV is near the leading edge at part-load flow rate condition (Q/QBEP= 0.85), and it moves towards the trailing edge to approximately 20% blade chord at the design flow rate condition (Q/QBEP= 1.0).